Damage tolerance modelling of fibre/metal laminate fuselage structures

Collection of Technical Papers - AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference

Volumn 4, Issue , 1997, Pages 2809-2818

  Langelaan, Jack W ^a   Kok, Leo J J ^a  

^a De Havilland Inc   (Canada)

Author keywords

[No Author keywords available]

Indexed keywords

COMPOSITE STRUCTURES; CRACK PROPAGATION; FAILURE ANALYSIS; FIBER REINFORCED METALS; FITS AND TOLERANCES; FUSELAGES; LAMINATED COMPOSITES; MATHEMATICAL MODELS; STRENGTH OF MATERIALS; STRESS INTENSITY FACTORS; STRUCTURAL ANALYSIS; STRUCTURAL LOADS;

DAMAGE TOLERANCE ANALYSIS; DISPLACEMENT COMPATIBILITY METHOD; RESIDUAL STRENGTH CURVES;

STRUCTURAL PANELS;

EID: 0030694899     PISSN: 02734508     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (16)